关键词: 进气道;发动机;性能;匹配;计算方法

Abstract: A method for calculation of cooperating point of inlet and engine according to testing data of inlet performance and flow performance of engine is presented in the paper. By the method, performance data of inlet can be precisely calculated in any flight condition and engine throttle. Compared with the graphic method used widely at present, the method in the paper can be used to set a mathematical model based on inlet performance data from wind tunnel test and given engine performance as well as working efficiency is raised and inlet performance data by calculating metod is more precise.

Key words: Inlet;Engine;Performance;Macthing;Computation method